CA2133992C - Compressing gas flowing through a conduit - Google Patents

Compressing gas flowing through a conduit Download PDF

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Publication number
CA2133992C
CA2133992C CA 2133992 CA2133992A CA2133992C CA 2133992 C CA2133992 C CA 2133992C CA 2133992 CA2133992 CA 2133992 CA 2133992 A CA2133992 A CA 2133992A CA 2133992 C CA2133992 C CA 2133992C
Authority
CA
Canada
Prior art keywords
conduit
return
valve
inlet valve
inlet
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA 2133992
Other languages
French (fr)
Other versions
CA2133992A1 (en
Inventor
Stephen G. Bryce
Leslie C. Shirvill
Christopher Morley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shell Canada Ltd
Original Assignee
Shell Canada Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shell Canada Ltd filed Critical Shell Canada Ltd
Publication of CA2133992A1 publication Critical patent/CA2133992A1/en
Application granted granted Critical
Publication of CA2133992C publication Critical patent/CA2133992C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C15/00Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B36/00Heating, cooling or insulating arrangements for boreholes or wells, e.g. for use in permafrost zones
    • E21B36/02Heating, cooling or insulating arrangements for boreholes or wells, e.g. for use in permafrost zones using burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F1/00Pumps using positively or negatively pressurised fluid medium acting directly on the liquid to be pumped
    • F04F1/06Pumps using positively or negatively pressurised fluid medium acting directly on the liquid to be pumped the fluid medium acting on the surface of the liquid to be pumped
    • F04F1/16Pumps using positively or negatively pressurised fluid medium acting directly on the liquid to be pumped the fluid medium acting on the surface of the liquid to be pumped characterised by the fluid medium being suddenly pressurised, e.g. by explosion
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/0318Processes
    • Y10T137/0391Affecting flow by the addition of material or energy

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Geology (AREA)
  • Fluid Mechanics (AREA)
  • Environmental & Geological Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Combustion & Propulsion (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Glass Compositions (AREA)

Abstract

Apparatus (1) for compressing gas, comprising a conduit (3) provided with a non-return inlet valve (10) arranged at the upstream inlet (5) end of the conduit (3), a localized ignition source (20) arranged in the conduit (3) downstream of the non-return inlet valve (10), and means (23) for intermittently supplying secondary fluid into the conduit (3) between the non-return inlet valve (10) and the localized ignition source (20).

Description

WO 93/21478 ~ ~ PCT/EP93/00962 COIKPRESSING GAS FLOWING THROUGH A CONDUIT
The present invention relates to compressing gas flowing through a conduit. The gas can be an inert gas or an oxidant or a combustible gas such as natural gas.
A suitable application of the present invention is downhole compression of natural gas; this is done to enhance the production from an underground natural gas reservoir. Natural gas is produced from an underground reservoir containing natural gas through a tubing arranged in a well drilled to the reservoir. During produc tion, the cumulative amount of natural gas produced increases and consequently thc~ reservoir pressure will decrease. As a result of the decrease in reservo it pressure the production rate decreases and, in order to maintain the production rate at an economically acceptable level. the gas has to be compressed, suitably the com-pression is donE: downho 1e. This compression also results in an increased economic cumulative production.
An alternative app:Lication of the present invention is com-pression of a gas flowing through a pipeline to increase the rate of gas transported through the pipeline.
USA patent specification No. 2 899 287 discloses an apparatus for compressing combustible gas comprising a conduit provided with a non-return inlet valve arranged at the upstream inlet end of the conduit, a localized i~mition source arranged in the conduit downstream of the non-return inlet valve, and means for supplying continuously fuel into the conduit between the non-return inlet valve and the localized ignition source.
The known ap~paratu~; is an apparatus for partially combusting fuel to generate a combustible gas. During normal operation, (a) fuel is supplied. continuously into the conduit to oxidant which has entered in the conduit through the non-return inlet valve; (b) the combustible mixture is allowed to ignite, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet end of the conduit and a low pressure wave front; and (c) the non-return inlet valve is allowed to open on arrival of the low pressure wave front to allow oxidant to enter into the conduit. Thereafter operation continues with the ~~teps (a) through (c).
In the known method the interval between two successive combustions is determined by the geometry of the conduit which may not always have the most suitable form for an optimal interval. The pressure increase for the compression stage of the known apparatus is very small, the pressure at the outlet end of the conduit is about 2 or 3 above the pressure at the inlet end. For pumping natural gas such a pressure increase for a compression stage is unacceptably small. Therefore it is an object of the present invention to provide an apparatus for compressing a gas which will give a larger pressure increase than the known apparatus.
To this end, apparatus for compressing gas according to an embodiment of the present invention comprises a conduit for carrying a gas provided with a non-return inlet valve arranged at an upstream inlet end of the conduit, a localized ignition source arranged in the conduit downstream of the non-return inlet valve, and means for intermittently supplying sect>ndary fluid into the conduit between the non-return inlet valve and the localized ignition source to form a combustible mixture, wherein the means for intermittently supplying secondary fluid comprises a container having an inlet provided with a restriction and an outlet debouching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet.
Another embodiment of the invention relates to a method of compressing a combustible gas flowing through a conduit having an inlet end and an outlet end and being provided with a non-return inlet valve at its inlet end, which method comprises the steps of (a) supplying intermittently oxidant into the conduit downstream of the non-return inlet valve, to form a combustible mixture, wherein means for intermittently supplying the oxidant comprises a container having <~n inlet provided with a restriction and an outlet debauching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet; (b) igniting the combustible mixture, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet end of the conduit and a low pressure wave front;
and (c) allowing the non-return inlet valve to open on arrival of the low pressure wave front to allow gas to enter into the conduit, followed by steps (a) through (c).
A further embodiment of the invention relates to a method of compressing oxidant flowing through a conduit having an inlet end and an outlet end and being provided with a non-return inlet valve at its inlet end, which method comprises the steps of (a) supplying intermittently a fuel-containing fluid into the conduit downstream of the non-return inlet valve to form a combustible mixture, wherein means for intermittently supplying the fuel-containing fluid comprises a container having an inlet provided with a restriction and an outlet debauching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet; (b) igniting the combustible mixture, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet end of the conduit and a low pressure wave front;

- 3a -and (c) allowing the non-return inlet valve to open on arrival of the low pressure wave front to allow gas to enter into the conduit, followed by steps (a) through (c).
Applicant has found that it is advantageous to supply intermittently a combustible mixture in the conduit, so that the interval between t:wo successive combustions is determined by the interval bet=ween successive supplies of combustible mixture in the conduit. The geometry of the conduit can now be selected to minimize the resistance to to flow.
By supplying intermittently a combustible mixture in the conduit the time-averaged amount of combustible mixture is small compared to the amount of gas flowing through the conduit.
The invention will now be described by way of example in more detail with reference to the accompanying drawing showing schematically a cross-sectional view of the apparatus for compressing gas according to the invention.
The apparatus 1 comprises a conduit 3 having an inlet end 5 and an outlet end 8, which conduit 3 is provided with a non-return inlet valve 10 arranged at the inlet end 5 of the conduit 3.
The conduit 3 is provided with a localized ignition source 20 arranged in the conduit 3 downstream of the non-return inlet valve 10, and with means 23 for intermittently supplying secondary fluid into the conduit 3 between the non-return inlet valve 10 and the localized ignition source 20.
The means 23 for intermittently supplying secondary fluid includes a container 26 having an inlet 27 - 3b -and an outlet 29 debouching into the conduit 3 provided with a non-return outlet valve 32, and a supply conduit 35 which is connected to the inlet 27.
When the gas to be compressed is a combustible gas, compressing such a gas using the apparatus according the present invention comprises allowing combustible gas to pass the non-return inlet valve 10 and supplying intermittently oxidant into the conduit through outlet 29 of the means 23 for intermittently supplying secondary fluid so that a combustible mixture is supplied ~z~'~3~~~~
intermittently in the conduit 3 downstream of the non-return inlet valve 10. The combustible mixture is allowed to ignite, which ignition yields a high pressure wave front closing the non-return inlet valve and. pushing gas out of the outlet end of the conduit , and a low pressure wave front. The non-return.-valve 10 is allowed to open on arrival of the low pressure wave-front to allow combus-tible gas to enter into the conduit 3. A grew cycle then starts.
The time-averaged amount of combustii~le gas required for the combustion is small compared to the amount of combustible gas flowing through the conduit 3.
This application is useful to compress natural gas for pumping the gas through a pipeline or through a well tubing arranged in a well extending from an. underground gas reservoir to surface.
The apparatus according to the invention can as well be used to compress oxidant, in which case the method comprises allowing oxidant to pass the non-return inlet valve 10 and supplying inter-mittently fuel into the conduit through outlet 29 so that a com-bustible mixture is supplied intermittently in the conduit 3 downstream of t:he non-return inlet valve 10. The combustible mixture is allowed to ignite, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet evnd of the conduit and a low pressure wave front. The non-return valve 10 is allowed to open on arrival of the low pressure wave front to allow combustible gas to enter into the conduit 3. A new cycle then starts.
When the localized ignition source 20 is sufficiently heated, the localized ignition source acts as a hot spot so that supply of electric power can be interrupted.
The oxidant is a gas containing free oxygen, an example of suitable oxidant is air, a further example is air enriched with oxygen. The oxidant can furthermore contain water, which upon vaporizing will furthermore increase the pressure.
Each of the non-return inlet valve 10 and the non-return outlet valve 32 can be provided with a control device (not shown) allowing opening of the each of the valves 10 and 32 at a pre-determined WO 93/21478 ~ ~ j 3 9 9 2 PCT/EP93/00962 pressure differE~nce across the valve. By adjusting the control device the opening characteristics of the non-return valves can be adjusted. An ex<<mple oj' such a control device is a spring, an other example of such a control device is a magnetic latch.
The interval. between two successive supplies of combustible mixture in the conduit is determined by the ratio of the diameter of the supply conduit :f5 and the inlet 27 of the container 26, the volume of the container 26, and the opening characteristics of the non-return outlea valve: 32.
It will be appreciated that more than one apparatus according to the present invention can be arranged in series, each following apparatus compressing t:he gas compressed by the previous one. If required, the compressed gas can be cooled between two successive compression stages.
The conduit 3 has a. constant inner diameter; in an alternative embodiment of the invention, the conduit comprises in the direction of flow a narrowing section upstream of the non-return valve 10, a section having a constant diameter and a widening section down-stream of the localized. ignition source 20.

Claims (5)

CLAIMS:
1. Apparatus for compressing gas, comprising a conduit for carrying a gas provided with a non-return inlet valve arranged at an upstream inlet end of the conduit, a localized ignition source arranged in the conduit downstream of the non-return inlet valve, and means for intermittently supplying secondary fluid into the conduit between the non-return inlet valve and the localized ignition source to form a combustible mixture, wherein the means for intermittently supplying secondary fluid comprises a container having an inlet provided with a restriction and an outlet debouching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet.
2. Apparatus according to claim 1, wherein the non-return outlet valve is provided with a control device allowing opening the outlet valve at a pre-determined pressure difference across the valve.
3. Apparatus according to claim 1 or 2, wherein the non-return inlet valve is provided with a control device allowing opening the inlet valve at a pre-determined pressure difference across the valve.
4. Method of compressing a combustible gas flowing through a conduit having an inlet end and an outlet end and being provided with a non-return inlet valve at its inlet end, which method comprises the steps of (a) supplying intermittently oxidant into the conduit downstream of the non-return inlet valve, to form a combustible mixture, wherein means for intermittently supplying the oxidant comprises a container having an inlet provided with a restriction and an outlet debouching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet;
(b) igniting the combustible mixture, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet end of the conduit and a low pressure wave front; and (c) allowing the non-return inlet valve to open on arrival of the low pressure wave front to allow gas to enter into the conduit, followed by steps (a) through (c).
5. Method of compressing oxidant flowing through a conduit having an inlet end and an outlet end and being provided with a non-return inlet valve at its inlet end, which method comprises the steps of (a) supplying intermittently a fuel-containing fluid into the conduit downstream of the non-return inlet valve to form a combustible mixture, wherein means for intermittently supplying the fuel-containing fluid comprises a container having an inlet provided with a restriction and an outlet debouching into the conduit provided with a non-return outlet valve, and a supply conduit connected to the inlet;
(b) igniting the combustible mixture, which ignition yields a high pressure wave front closing the non-return inlet valve and pushing gas out of the outlet end of the conduit and a low pressure wave front; and (c) allowing the non-return inlet valve to open on arrival of the low pressure wave front to allow gas to enter into the conduit, followed by steps (a) through (c).
CA 2133992 1992-04-22 1993-04-19 Compressing gas flowing through a conduit Expired - Fee Related CA2133992C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP92201141 1992-04-22
EP92201141.6 1992-04-22
PCT/EP1993/000962 WO1993021478A1 (en) 1992-04-22 1993-04-19 Compressing gas flowing through a conduit

Publications (2)

Publication Number Publication Date
CA2133992A1 CA2133992A1 (en) 1993-10-28
CA2133992C true CA2133992C (en) 2004-06-29

Family

ID=8210572

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2133992 Expired - Fee Related CA2133992C (en) 1992-04-22 1993-04-19 Compressing gas flowing through a conduit

Country Status (10)

Country Link
US (1) US5391057A (en)
EP (1) EP0636229B1 (en)
AU (1) AU671993B2 (en)
CA (1) CA2133992C (en)
DE (1) DE69306104T2 (en)
DK (1) DK0636229T3 (en)
MY (1) MY108859A (en)
NO (1) NO302591B1 (en)
NZ (1) NZ251979A (en)
WO (1) WO1993021478A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2133989C (en) * 1992-04-22 2004-08-10 Egbert Leonardus Cox Compressing combustible gas flowing throughout a conduit
US7891960B2 (en) 2006-03-13 2011-02-22 Lea Jr James F Reciprocal pump for gas and liquids
US11073168B2 (en) * 2017-02-21 2021-07-27 Raymond C. Vaughan Compressor having elliptically-shaped combustion chambers with fuel injection and ignition occurring at the foci

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899287A (en) * 1959-08-11 Gas producer with
US355116A (en) * 1886-12-28 Egbert slade ash
US3257180A (en) * 1966-06-21 Vapor injection system
US2192011A (en) * 1937-06-30 1940-02-27 Koller Karl Apparatus for preventing condensation in gas mains
US2398654A (en) * 1940-01-24 1946-04-16 Anglo Saxon Petroleum Co Combustion burner
US2614387A (en) * 1946-09-17 1952-10-21 Ingersoll Rand Co Intermittent explosion unit for gas turbine plants
US2636445A (en) * 1946-12-27 1953-04-28 Fred S Tutton Production method and apparatus
US2550515A (en) * 1947-11-19 1951-04-24 Ingersoll Rand Co Gas compressor
FR1011313A (en) * 1949-01-15 1952-06-23 Brev Tamassy Soc D Expl Des Device for causing water to move
US2719080A (en) * 1951-10-23 1955-09-27 Edwin X Schmidt Gas mixing control methods and apparatus
US2860484A (en) * 1956-06-04 1958-11-18 Schmidt Paul Apparatus for causing intermittent combustion of a fuel in a chamber as a means of producing useful energy
US3112988A (en) * 1960-02-26 1963-12-03 Sheil Oil Company Mixing gases at supersonic velocity
US3108737A (en) * 1962-03-26 1963-10-29 Denver R King Air compressor
DE2347129A1 (en) * 1973-09-19 1975-03-27 Otto Tuchenhagen Compressed gas producer by internal combustion - has ignition controlled by pressure sensor in takeoff pipe
DE2700044A1 (en) * 1977-01-03 1978-07-06 Didier Eng METHOD FOR PREVENTING CONDENSATION DURING THE TRANSPORT OF HOT COOKING RAW GASES TO THE APPLICATION POINT
NL7807184A (en) * 1977-07-18 1979-01-22 Caloric Ges Apparatebau METHOD AND INSTALLATION FOR TRANSPORTING REAL GASES, ESPECIALLY NATURAL GAS.
US4860484A (en) * 1986-07-14 1989-08-29 Green Milton J Reel seat structures for fishing rods
CA2133989C (en) * 1992-04-22 2004-08-10 Egbert Leonardus Cox Compressing combustible gas flowing throughout a conduit

Also Published As

Publication number Publication date
NO943978D0 (en) 1994-10-20
NO943978L (en) 1994-10-20
NO302591B1 (en) 1998-03-23
EP0636229B1 (en) 1996-11-20
AU671993B2 (en) 1996-09-19
MY108859A (en) 1996-11-30
DE69306104T2 (en) 1997-05-28
WO1993021478A1 (en) 1993-10-28
NZ251979A (en) 1996-04-26
US5391057A (en) 1995-02-21
AU4040793A (en) 1993-11-18
CA2133992A1 (en) 1993-10-28
DE69306104D1 (en) 1997-01-02
DK0636229T3 (en) 1997-05-05
EP0636229A1 (en) 1995-02-01

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